As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT WING UPPER SURFACE FROM XW 468 TO WING TIP, HAS SURFACE CORROSION FORMING IN MULTIPLE AREAS. PERFORMED UT INSPECTION & CORROSION DETECTED. PERFORMED BLEND OUT. PERFORMED NDT, DP & HFEC OPEN HOLE INSPECTIONS. BLEND OUT OF LIMITS. FABRICATED REPAIR DOUBLER & INSTALLED IAW EA 008-5730-38-A6030.